Cessna 402C - Page 134

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TIME, FUEL AND DISTANCE TO CLIMB - MAXIMUM CLIMB
ac -40 -30 -20 -10 0 10 20 30 40 50
I I I ! I I I I I )
I I I I I I I I
OF -40 -20 0 20 40 60 80 100 120
OUTSIDE AIR TEMPERATURE
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NOTE:
1. Time. Fuel and
Distance for the Climb
are Determined by
Taking the Difference
Between the Airport
Altitude and Initial
Cruise.
2.
For Total Fuel Used,
Add 35 Pounds for
Start, Taxi and
Takeoff
CONDITIONS:
1. 2600 RPM and 39.0
Inches Hg.*
2. Mixture - Check Fuel
Flow In White Triangle.*
3. Landing Gear - UP.
4. Wing Flaps - UP.
5. Cowl Flaps - OPEN.
*Above 16.000 Feet. Use
Placarded Manifold
Pressure and Climb Fuel
Flow.
WEIGHT-
CLIMB SPEED
POUNDS
- KIAS
6850
109
6500
106
6000
102
5500
97
5000
92
o 5 10 15 20 25 30
TIME TO CLIMB - MINUTES
1 ! ! I ! I I
r I I , i I I I I I iii
o 20 40 60 80 100 120 140
FUEL TO CLIMB - POUNDS
I 1 I I ! I I
I I i I I I i
o 10 20 30 40 50 60 70
DISTANCE TO CLIMB - NAUTICAL MILES (ZERO WIND)
Figure 5-18
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4
2
26
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